CN106275435B - A kind of jet-propelled manned vehicle - Google Patents
A kind of jet-propelled manned vehicle Download PDFInfo
- Publication number
- CN106275435B CN106275435B CN201610804435.0A CN201610804435A CN106275435B CN 106275435 B CN106275435 B CN 106275435B CN 201610804435 A CN201610804435 A CN 201610804435A CN 106275435 B CN106275435 B CN 106275435B
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- Prior art keywords
- plate
- articulated slab
- flight
- parallel
- electric cylinders
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
The present invention discloses a kind of jet-propelled manned vehicle, including flight seat, two elastic buffer framves, four featured rockets, hand steered arm and operation handle, two sets of side flight systems, rear portion turbojet engine, battery, two elastic buffer framves are symmetrically mounted on flight seat lower part；Four featured rockets are mounted on flight seat lower part；Side flight system is respectively symmetrically mounted on flight seat two sides, big parallel-plate is mounted on flight seat side, the side of upper articulated slab and lower articulated slab, which is respectively articulated with, to be mounted on big parallel-plate, the other side of upper articulated slab and lower articulated slab is hingedly equipped with small parallel-plate, and small parallel-plate is parallel to each other with big parallel-plate；The cylinder ends of articulated slab adjustment electric cylinders are hingedly mounted on big parallel-plate lower part, and the piston rod end of engine adjustment electric cylinders is hingedly mounted on the turbojet engine of side.The present invention realizes the purpose of freely easy operation flight by being provided with multi-angle adjustable flight system；The configuration of the present invention is simple, it is easy to operate.
Description
Technical field
The present invention relates to vehicle technology field, in particular to a kind of jet-propelled manned vehicle.
Background technique
In actual life, the trip of people relies on the vehicles mostly, and for the trip of short distance especially pavement behavior
In the case where difference, conventional vehicles volume is larger, and expense is more expensive, when passing through inconvenient barrier and detour bring
Between it is long the problems such as, it is therefore desirable to a kind of time saving and energy saving vehicles of short distance trip.
Summary of the invention
In view of the above-mentioned problems, the present invention provides a kind of jet-propelled manned vehicle, it is adjustable by being provided with multi-angle
Formula flight system realizes the purpose of freely easy operation flight.
Technical solution used in the present invention is: a kind of jet-propelled manned vehicle, including flight seat, two elasticity are slow
Frame, four featured rockets, hand steered arm and operation handle, two sets of side flight systems, rear portion turbojet engine, battery are rushed, it is special
Sign is: two elastic buffer framves are symmetrically mounted on flight seat lower part；Four featured rockets are mounted on winged
Row seat lower part；The hand steered arm is mounted on flight seat side, and the operation handle is mounted on hand steered arm；Described
Rear portion turbojet engine is mounted on flight seat rear；The battery is mounted on flight seat rear, and is located at rear portion whirlpool and sprays
Above engine；The side flight system is respectively symmetrically mounted on flight seat two sides, and side flight system includes: big flat
Andante and small parallel-plate, upper articulated slab and lower articulated slab, articulated slab adjustment electric cylinders, rotating electric machine and swivel mount, the eruption of side whirlpool
Motivation, engine adjust electric cylinders, and the big parallel-plate is mounted on flight seat side, the upper articulated slab and lower articulated slab
Side be respectively articulated with and be mounted on big parallel-plate, the other side of upper articulated slab and lower articulated slab is hingedly equipped with small parallel-plate,
The small parallel-plate is parallel to each other with big parallel-plate；The cylinder ends of the articulated slab adjustment electric cylinders are hingedly mounted on big flat
The end of andante lower part, the piston rod of articulated slab adjustment electric cylinders is hingedly mounted on lower articulated slab lower part；The rotating electric machine peace
On small parallel-plate, swivel mount is installed on rotating electric machine main shaft, the side turbojet engine is hingedly mounted on rotation
On frame；The cylinder ends of the engine adjustment electric cylinders are hingedly mounted on swivel mount lower part, and engine adjusts the piston of electric cylinders
Boom end is hingedly mounted on the turbojet engine of side.
Since present invention employs above-mentioned technical proposals, the invention has the following advantages that the present invention is polygonal by being provided with
Adjustable flight system is spent, the purpose of freely easy operation flight is realized；The configuration of the present invention is simple, it is easy to operate.
Detailed description of the invention
Fig. 1 is overall structure diagram of the invention.
Fig. 2 is the overall structure diagram of another angle of the present invention.
Fig. 3 is the overall structure diagram of another angle of the present invention.
Drawing reference numeral: 1- flight seat；2- promotes mainly rocket；The small parallel-plate of 3-；4- articulated slab adjusts electric cylinders；5- elastic buffer
Frame；The hand steered arm of 6-；7- operation handle；The big parallel-plate of 8-；Articulated slab under 9-；The upper articulated slab of 10-；11- rotating electric machine；12- starts
Machine adjusts electric cylinders；13- swivel mount；The side 14- turbojet engine；The rear portion 15- turbojet engine；16- battery.
Specific embodiment
The invention will be further described combined with specific embodiments below, in the illustrative examples and explanation of the invention
For explaining the present invention, but it is not as a limitation of the invention.
As shown in Figure 1, Figure 2, Figure 3 shows, a kind of jet-propelled manned vehicle, including 1, two elastic buffer frame 5 of flight seat,
Four featured rockets 2, hand steered arm 6 and operation handle 7, two sets of side flight systems, rear portion turbojet engine 15, batteries 1.Two
Elastic buffer frame 5 is symmetrically mounted on 1 lower part of flight seat.Four featured rockets 2 are mounted on 1 lower part of flight seat.Hand steered arm 6 is pacified
Mounted in 1 side of flight seat, operation handle 7 is mounted on hand steered arm 6.After rear portion turbojet engine 15 is mounted on flight seat 1
Portion.Battery 16 is mounted on 1 rear portion of flight seat, and is located at 15 top of rear portion turbojet engine.Side flight system is respectively symmetrically
It is mounted on 1 two sides of flight seat, side flight system includes: big parallel-plate 8 and small parallel-plate 3, upper articulated slab 10 and lower hinged
Plate 9, articulated slab adjustment electric cylinders 4, rotating electric machine 11 and swivel mount 13, side turbojet engine 14, engine adjust electric cylinders 12, greatly
Parallel-plate 8 is mounted on 1 side of flight seat, and the side of upper articulated slab 10 and lower articulated slab 9, which is respectively articulated with, is mounted on big parallel-plate 8
On, the other side of upper articulated slab 10 and lower articulated slab 9 is hingedly equipped with small parallel-plate 3, and small parallel-plate 3 and big parallel-plate 8 are mutual
In parallel.The cylinder ends of articulated slab adjustment electric cylinders 4 are hingedly mounted on big 8 lower part of parallel-plate, and articulated slab adjusts the piston rod of electric cylinders 4
End be hingedly mounted on lower 9 lower part of articulated slab.Rotating electric machine 11 is mounted on small parallel-plate 3, is installed on 3 main shaft of rotating electric machine
There is swivel mount 13, side turbojet engine 14 is hingedly mounted on swivel mount 13.Engine adjusts the cylinder ends hinge of electric cylinders 12
It connects and is mounted on 13 lower part of swivel mount, the piston rod end of engine adjustment electric cylinders 12 is hingedly mounted on side turbojet engine 14
On.
Working principle of the present invention: in the use of the present invention, can adjust electric cylinders 4 by articulated slab adjusts upper 10 He of articulated slab
The height and angle of rotating electric machine 11 can be adjusted in the height and angle of lower articulated slab 9；Pass through the adjustable side of rotating electric machine 11
The angle of portion's turbojet engine 14；The tilt angle of the adjustable side turbojet engine 14 of electric cylinders 12 is adjusted by engine；
The present invention can further provide for power by rear portion turbojet engine 15；The featured rocket 2 of 1 lower part of flight seat can be in side
For the present invention further provides power when portion's turbojet engine 14 and rear portion turbojet engine 15 fail；Two elastic buffer framves 5
It can play the role of buffering in present invention landing.
Claims (1)
1. a kind of jet-propelled manned vehicle, including flight seat (1), two elastic buffer framves (5), four featured rockets (2),
Hand steered arm (6) and operation handle (7), two sets of side flight systems, rear portion turbojet engine (15), battery (16), feature exists
In: two elastic buffer framves (5) are symmetrically mounted on flight seat (1) lower part；Featured rocket (2) installation of described four
In flight seat (1) lower part；The hand steered arm (6) is mounted on flight seat (1) side, the operation handle (7) installation
On hand steered arm (6)；The rear portion turbojet engine (15) is mounted on flight seat (1) rear portion；Battery (16) peace
Mounted in flight seat (1) rear portion, and it is located above rear portion turbojet engine (15)；The side flight system is respectively symmetrically pacified
Mounted in flight seat (1) two sides, side flight system include: big parallel-plate (8) and small parallel-plate (3), upper articulated slab (10) and
Lower articulated slab (9), articulated slab adjustment electric cylinders (4), rotating electric machine (11) and swivel mount (13), side turbojet engine (14), hair
Motivation adjusts electric cylinders (12), and the big parallel-plate (8) is mounted on flight seat (1) side, the upper articulated slab (10) and
The side of lower articulated slab (9), which is respectively articulated with, to be mounted on big parallel-plate (8), upper articulated slab (10) and lower articulated slab (9) it is another
Side is hingedly equipped with small parallel-plate (3), and the small parallel-plate (3) is parallel to each other with big parallel-plate (8)；The articulated slab tune
The cylinder ends of whole electric cylinders (4) are hingedly mounted on big parallel-plate (8) lower part, and articulated slab adjusts the end of the piston rod of electric cylinders (4)
It is hingedly mounted on lower articulated slab (9) lower part；The rotating electric machine (11) is mounted on small parallel-plate (3), rotating electric machine (11)
It is equipped on main shaft swivel mount (13), the side turbojet engine (14) is hingedly mounted on swivel mount (13)；Described
The cylinder ends of engine adjustment electric cylinders (12) are hingedly mounted on swivel mount (13) lower part, and engine adjusts the piston of electric cylinders (12)
Boom end is hingedly mounted on side turbojet engine (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610804435.0A CN106275435B (en) | 2016-09-06 | 2016-09-06 | A kind of jet-propelled manned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610804435.0A CN106275435B (en) | 2016-09-06 | 2016-09-06 | A kind of jet-propelled manned vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106275435A CN106275435A (en) | 2017-01-04 |
| CN106275435B true CN106275435B (en) | 2018-12-04 |
Family
ID=57710744
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610804435.0A Active CN106275435B (en) | 2016-09-06 | 2016-09-06 | A kind of jet-propelled manned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106275435B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| PL428928A1 (en) * | 2019-02-15 | 2020-08-24 | Zbigniew Władysław Mazurkiewicz | Aviation engine power unit with accessories and power supply |
| GB2614228B (en) * | 2021-10-21 | 2023-12-20 | Maverick Aviation Ltd | A VTOL aerial vehicle |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1114831A (en) * | 1993-09-21 | 1996-01-10 | 贝尔创新创办公司 | Flight device |
| WO2003039700A1 (en) * | 2001-11-07 | 2003-05-15 | Aerodavinci Co., Ltd. | Compressed air engine and flying object equipped therewith |
| CN204473140U (en) * | 2015-03-05 | 2015-07-15 | 华北电力大学科技学院 | New vertical landing tilting rotor two axle aircraft |
| CN104908937A (en) * | 2015-06-30 | 2015-09-16 | 孙建香 | Agricultural sprayer |
| CN105000176A (en) * | 2015-08-10 | 2015-10-28 | 徐金鹏 | Jet aircraft |
-
2016
- 2016-09-06 CN CN201610804435.0A patent/CN106275435B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1114831A (en) * | 1993-09-21 | 1996-01-10 | 贝尔创新创办公司 | Flight device |
| WO2003039700A1 (en) * | 2001-11-07 | 2003-05-15 | Aerodavinci Co., Ltd. | Compressed air engine and flying object equipped therewith |
| CN204473140U (en) * | 2015-03-05 | 2015-07-15 | 华北电力大学科技学院 | New vertical landing tilting rotor two axle aircraft |
| CN104908937A (en) * | 2015-06-30 | 2015-09-16 | 孙建香 | Agricultural sprayer |
| CN105000176A (en) * | 2015-08-10 | 2015-10-28 | 徐金鹏 | Jet aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106275435A (en) | 2017-01-04 |
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| Date | Code | Title | Description |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181024 Address after: 402660 Chongqing Tongnan District Zitong Subdistrict Office, No. 6, No. 2 workshop Applicant after: Kang Kang robot (Chongqing) Co., Ltd. Address before: 054999 101 Yao Lou village, Luzhai Township, Linxi County, Xingtai, Hebei Applicant before: Xu Hongen |
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| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |